Design and Predictions for High-Altitude (Low Reynolds Number) Aerodynamic Flight Experiment

Author:

Greer Donald1,Hamory Phil1,Krake Keith2,Drela Mark3

Affiliation:

1. NASA Dryden Flight Research Center, Edwards, California 93523

2. Sparta, Inc., Edwards, California 93523

3. Massachusetts Institute of Technology, Cambridge, Massachusetts 02139

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

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2. Dynamics simulation of a folding wing unmanned aerial vehicle with the parachute system assisted launching;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-09-06

3. Circulation dynamics of small-amplitude pitching airfoil undergoing laminar-to-turbulent transition;Journal of Fluids and Structures;2021-01

4. Development of a testing methodology for high-altitude propeller;Aircraft Engineering and Aerospace Technology;2018-10-19

5. Aerofoil Design for Unmanned High-Altitude Aft-Swept Flying Wings;Journal of Aerospace Technology and Management;2017-08-03

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